LEADER 01548nam  2200445Ia 450 
001 9910698893003321
005 20090505110933.0
035   $a(CKB)5470000002396931
035   $a(OCoLC)320242426
035   $a(EXLCZ)995470000002396931
100   $a20090505d1989      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA method of isolating treadmill shock and vibration on spacecraft$b[electronic resource] /$fWilliam E. Thornton
210  1$aHouston, Tex. :$cNational Aeronautics and Space Administration, Lyndon B. Johnson Space Center,$d[1989]
215   $a15 pages $cdigital, PDF file
225 1 $aNASA technical memorandum ;$v100474
300   $aTitle from title screen (viewed May 4, 2009)
300   $a"April 1989."
320   $aIncludes bibliographical references (page 3).
606   $aShock resistance$2nasat
606   $aSpacecraft design$2nasat
606   $aTreadmills$2nasat
606   $aVibration isolators$2nasat
606   $aVibration tests$2nasat
615  7$aShock resistance.
615  7$aSpacecraft design.
615  7$aTreadmills.
615  7$aVibration isolators.
615  7$aVibration tests.
700   $aThornton$b William E$g(William Edgar),$f1929-$01410970
712 02$aLyndon B. Johnson Space Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910698893003321
996   $aA method of isolating treadmill shock and vibration on spacecraft$93500991
997   $aUNINA